Hughes 269 (H269)
ICAO H269 Light

Hughes 269

Single Rotorcraft

The Hughes 269 is a lightweight two-seat piston helicopter that became one of the most successful training helicopters in aviation history. First flown in 1956, it was designed by Howard Hughes' aircraft division as a simple, rugged trainer with docile handling characteristics that made it ideal for ab-initio rotorcraft instruction. The U.S. Army adopted it as the TH-55 Osage in 1964, training thousands of Vietnam-era pilots on the type, and civilian flight schools worldwide embraced it for its low operating costs and forgiving flight envelope. The 269 features a three-blade main rotor, a piston Lycoming HIO-360 engine producing 190 horsepower, and an aluminum semi-monocoque fuselage with excellent visibility from its bubble canopy. Its never-exceed speed of 86 knots and service ceiling around 10,200 feet made it modest in performance but perfectly suited to the training mission, where predictability mattered more than speed. After Hughes left the helicopter business, production continued under Schweizer Aircraft as the 300 series from 1983 onward, with the 300C and 300CBi variants adding fuel injection and minor refinements while preserving the original's straightforward design philosophy. The type remains in service today at flight schools, for pipeline patrol, and in private hands, valued for its mechanical simplicity and relatively low maintenance burden compared to turbine trainers. SkyMeter has tracked 105 flights across 34 airframes and 23 operators, with HOUSTON POLICE DEPT, AIR SUPPORT DIV the largest observed operator.

ACTIVE AIRFRAMES
34
last 7 days
🏢
OPERATORS
23
unique airlines
📊
FLIGHTS
105
tracked
AVG DURATION
1h 0m
per flight
INCIDENT RATE
6.7%
7 flagged

Safety in context

The incident rate counts flights with ANY safety event detected by SkyMeter: go-arounds (a routine response, not a failure), unstable-approach gate flags (advisory thresholds), rejected takeoffs (the system working as designed), and runway events. It is NOT an accident rate or fatality rate. For accident statistics, refer to the NTSB Aviation Accident Database (USA) or the Aviation Safety Network. See methodology for what each event type measures.

Performance

Speed envelope & approach

Vref
Vref range
Vmo
Mmo
Approach category

Dimensions

Airframe geometry

Wingspan
Length
Tail height
Wheelbase
Gear width
Wake category
L

Weight & identification

Operating limits

MTOW
1,850 lb
MALW
Manufacturer model
269
FAA designator
Registered

Recent incidents

Flagged flights of H269

20
8/14/2026
34m
△ Low approach-stability score
8/12/2026
55m
△ Low approach-stability score
8/12/2026
33m
△ Low approach-stability score
8/7/2026
44m
△ Low approach-stability score
8/5/2026
32m
△ Low approach-stability score
7/30/2026
1h 20m
△ Low approach-stability score
7/24/2026
54m
△ Low approach-stability score
7/24/2026
47m
△ Low approach-stability score
7/24/2026
24m
△ Low approach-stability score
7/23/2026
1h 24m
△ Low approach-stability score

Recent flights

Real flights of H269 · airborne ≥ 20 min

30
8/15/2026
35m
No alerts
8/15/2026
38m
No alerts
8/15/2026
25m
No alerts
8/15/2026
28m
No alerts
8/15/2026
21m
No alerts
8/15/2026
3h 54m
No alerts
8/15/2026
34m
No alerts
8/15/2026
49m
No alerts
8/15/2026
57m
No alerts
8/15/2026
37m
No alerts
8/15/2026
55m
No alerts
8/15/2026
19m
No alerts
8/15/2026
1h 3m
No alerts
8/14/2026
29m
No alerts
8/14/2026
22m
No alerts
8/14/2026
25m
No alerts
8/14/2026
1h 19m
No alerts
8/14/2026
40m
No alerts
8/14/2026
1h 1m
No alerts
8/14/2026
34m
△ Low approach-stability score
8/14/2026
1h 14m
No alerts
8/14/2026
38m
No alerts
8/14/2026
42m
No alerts
8/14/2026
4h 32m
No alerts
8/14/2026
57m
No alerts
8/14/2026
39m
No alerts
8/14/2026
45m
No alerts
8/14/2026
23m
No alerts
8/14/2026
44m
No alerts
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© SkyMeter · All flight data subject to ODbL attribution · Tracking window: 7 days (free tier)